大气层外拦截变结构导引律

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1996, Vol. 17 ›› Issue (2): 155-161.

• 论文 • Previous Articles Next Articles

VARIABLE STRUCTURE GUIDANCE LAW FOR EXTRA-ATMOSPHERIC INTERCEPTION

Wang Jiayun, Er Lianjie, Wu Wenzheng, Wang Xiaodong

Beijing University of Aeronautics and Astronautics, Beijing,100083

Received:1993-06-01 Revised:1994-11-01 Online:1996-04-25 Published:1996-04-25

Abstract

Abstract: The variable structure guidance law of extra atmospheric interception is studied. Inorder to eliminate the effects of outer and systematic perturbation and disturbance, a guidance law based on the variable structure control theory with a strong robustness is proposed. The coefficient matrix of the switching function is determined by the concept of zero control interception. The asymptotic law which guarantees the quality of transient process before reaching the switching surface is used in practice. The results of digital simulation and comparison with the proportional and optimal guidance laws are included.

Key words: extraatmo spheric interception, variable structure, guidance law

CLC Number:

V212112

Wang Jiayun;Er Lianjie;Wu Wenzheng;Wang Xiaodong. VARIABLE STRUCTURE GUIDANCE LAW FOR EXTRA-ATMOSPHERIC INTERCEPTION[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(2): 155-161.

[1]	Ziyi WU, Shaoming HE, Yadong WANG, Hongyan LI. Nonlinear observability-enhancement optimal guidance law for moving targets [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729750-729750.
[2]	Yongzhi SHENG, Jiahao GAN, Chengxin ZHANG. Fractional order sliding mode guidance law design with trajectory adjustable and terminal angular constraint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 327073-327073.
[3]	WANG Yinhan, FAN Shipeng, WU Guang, WANG Jiang, HE Shaoming. Fast guidance law identification approach for incoming missile based on GRU network [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 325024-325024.
[4]	HE Lei, YAN Xiaodong, TANG Shuo. Guidance law design for spiral-diving maneuver penetration [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(5): 322457-322457.
[5]	LI Xiaobao, ZHAO Guorong, ZHANG Youan, GUO Zhiqiang. Adaptive nonsingular terminal sliding mode guidance law with strict convergence [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(5): 322569-322569.
[6]	ZHANG Kuanqiao, YANG Suochang, LI Baochen, LIU Chang. Fixed-time convergent guidance law considering autopilot dynamics [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(11): 323227-323227.
[7]	DUAN Meijun, ZHOU Di, CHENG Dalin. Development of terminal guidance law and PWPF modulator for near space interceptor based on finite time theory [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(1): 321481-321481.
[8]	GUO Jianguo, HAN Tuo, ZHOU Jun, WANG Guoqing. Second-order sliding-mode guidance law with impact angle constraint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(2): 320208-320217.
[9]	ZHAO Qilun, CHEN Jian, DONG Xiwang, LI Qingdong, REN Zhang. Cooperative guidance law for heterogeneous missiles intercepting hypersonic weapon [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(3): 936-948.
[10]	ZHANG Min, TIAN Pengfei, CHEN Xin. UAV guidance law for circumnavigating and tracking ground target and its stability proof [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(11): 3425-3434.
[11]	LI Yuan, YAN Liang, ZHAO Jiguang, CHEN Jingpeng. Method of time-to-go estimation for head-pursuit interception mode [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(9): 3082-3091.
[12]	YAN Liang, ZHAO Jiguang, SHEN Huairong, LI Yuan. Three-dimensional United Biased Proportional Navigation Guidance Law for Interception of Targets with Angular Constraints [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(7): 1999-2010.
[13]	LIU Pengyun, SUN Ruisheng, LI Weiming, MING Chao. A Coning Motion-based Guidance Law for Guided Rocket with Velocity Control [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(4): 933-941.
[14]	WU Nan, CHEN Lei. Adaptive Kalman Filtering for Trajectory Estimation of Hypersonic Glide Reentry Vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(8): 1960-1971.
[15]	WEI Wenshu, JING Wuxing, GAO Changsheng. Research Automatic Stability Technology of Spacecraft Assembly with Captured Non-cooperative Targets on Orbit [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(7): 1520-1530.

VARIABLE STRUCTURE GUIDANCE LAW FOR EXTRA-ATMOSPHERIC INTERCEPTION

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments